[fltsim.0] title=WB-57F USAF sim=WB-57F model=USAF panel= sound= texture=USAF kb_checklists= //ui_manufacturer=AJóR WFbg@ //ui_type=General Dynamics WB-57F Canberra ui_manufacturer=General Dynamics ui_type=WB-57F Canberra ui_variation=(01) USAF 63-13286 description=The primary user of the WB-57F was the 58th Weather Reconnaissance Squadron at Kirtland AFB, in Albuquerque, New Mexico, who received their first aircraft in 1964.\nThese Canberras were deployed throughout the world where there was suspected atmospheric testing of nuclear devices to sample the upper atmosphere for nuclear debris.\n\nby Kazunori Ito\n Kazu1664VT@aol.com [fltsim.1] title=WB-57F NASA sim=WB-57F model=NASA panel= sound= texture=NASA kb_checklists= //ui_manufacturer=AJóR WFbg@ //ui_type=General Dynamics WB-57F Canberra ui_manufacturer=General Dynamics ui_type=WB-57F Canberra ui_variation=(02) NASA 926 description=In 1968, NASA had contracted with the Air Force to operate an RB-57F, which flew many research missions as part of the Earth Resources Technology Satellite program. \nIn 1972, the Air Force thought the expense was too high, and transferred the plane to NASA. \nThis aircraft was re-numbered NASA 925. This plane operated until 1982\nWhen the 58th WRS high altitude program was cut in 1974, they also transferred NASA 926 to Houston. \nWhile this plane was out of service for some time due to budget considerations, it is still flying missions today, operating out of Ellington Field in Houston, Texas. More recently, NASA acquired another WB-57F, numbered NASA 928.\nNASA 926 and NASA 928 are the only two WB-57s still flying in the world today.\n\nby Kazunori Ito\n Kazu1664VT@aol.com [General] performance=Width: 37.34m (122 ft. 5 in.)\nLength: 20.76m (68 ft. 10 in.)\nHeight: 5.79m (19 ft. 0 in.) \nArmament: None (although the bomb bay could be converted to carry bombs if necessary)\nEngines: Two Pratt & Whitney TF33-P-11 turbofans of 16,000 lbs. static thrust each, plus two (removable) Pratt & Whitney J60-P-9 turbojets of 3,300 lbs. Static thrust each \nCrew: 2 - pilot and navigator/observer\n\nMaximum Speed: 550 mph / 475 knots \nRange: 4,000 miles / 3475 nautical miles\nService Ceiling: 82,000 ft. \n [pitot_static] vertical_speed_time_constant=100 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [WEIGHT_AND_BALANCE] max_gross_weight=180000 empty_weight=100000 reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI=3172439 empty_weight_roll_MOI=2262183 empty_weight_yaw_MOI=3337024 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=25.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=26400 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=0 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [contact_points] point.0=1, 40.00, 0.00, -8.10, 1181.1, 0, 1.442, 55.92, 0.8, 2.5, 0.9, 13.0, 13.0, 0, 0.0, 0.0 point.1=1, -7.75, -8.58, -8.68, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 13.0, 13.0, 2, 0.0, 0.0 point.2=1, -7.75, 8.58, -8.68, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 13.0, 13.0, 3, 0.0, 0.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 max_number_of_points=21 static_pitch=0.62 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.66 //feet, altitude of CG when at rest on the ground [Views] eyepoint=23.324721,0.000000,2.832288 [direction_indicators] direction_indicator.0=3,0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 150 aileron=150, 150 rudder=150, 150 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2200 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 use_no_default_bank=1 [airplane_geometry] wing_area=2137.0 //Square feet wing_span=94.75 //Feet wing_root_chord=18.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=-0.5 //Degrees oswald_efficiency_factor=0.75 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=25.0 //Degrees, wing leading edge wing_pos_apex_lon=8.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=338.0 //Square feet htail_span=41.7 //Feet htail_pos_lon=-35.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=224.0 //Square feet vtail_span=20.0 //Feet, tip to body vtail_sweep=35.0 //Degrees, vertical tail leading edge vtail_pos_lon=-35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=5.8 //Feet, vertical distance from reference point, positive going up elevator_area=70.5 //Square feet aileron_area=26.9 //Square feet rudder_area=56.2 //Square feet elevator_up_limit=22.5 //Degrees elevator_down_limit=19.5 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=20.0 //Degrees rudder_limit=26.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=60.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=142.0 //Knots True (KTAS) full_flaps_stall_speed=113.0 //Knots True (KTAS) cruise_speed=477.0 //Knots True (KTAS) [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [GeneralEngineData] engine_type=1 Engine.0=4.166667,-9.166667,-2.500000 Engine.1=4.166667,-8.333333,-2.500000 Engine.2=4.166667,8.333333,-2.500000 Engine.3=4.166667,9.166667,-2.500000 fuel_flow_scalar=0.324566 [fuel] Center1=0.000000,0.000000,0.000000,1000.000000,0.000000 LeftMain=0.000000,0.000000,0.000000,2500.000000,0.000000 LeftAux=0.000000,0.000000,0.000000,1000.000000,0.000000 RightMain=0.000000,0.000000,0.000000,2500.000000,0.000000 RightAux=0.000000,0.000000,0.000000,1000.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //6=taxi light, 7=recognition light, 8=wing light, 9=logo light // Z, X, Y light.0=3, -8.53, 0.00, 1.05, fx_navred , light.1=2, -8.53, 0.00, 1.05, fx_strobe , light.2=3, -4.40, 0.00, -5.31, fx_navred , light.3=2, -4.40, 0.00, -5.31, fx_strobe , light.4=3, 3.30, 60.63, -4.00, fx_navgre , light.5=2, 3.30, 60.63, -4.00, fx_strobe , light.6=3, 3.30, -60.63, -4.00, fx_navred , light.7=2, 3.30, -60.63, -4.00, fx_strobe , light.8=3, -34.09, 0.00, -0.97, fx_navwhi ,
